Fuselage sections (300) having tapered wing rib interfaces (306) are disclosed. A disclosed example apparatus includes a rib (306) associated with a fuselage section (300), and a wing interface surface defined by the rib (306), where the wing interface surface is tapered relative to a longitudinal axis (330) of the fuselage section from an aft end of the fuselage section (300) to a fore end of the fuselage section (300).


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    Title :

    FUSELAGE SECTIONS HAVING TAPERED WING RIB INTERFACES


    Additional title:

    RUMPFSEKTIONEN MIT KONISCHEN FLÜGELRIPPENSCHNITTSTELLEN
    SECTIONS DE FUSELAGE AYANT DES INTERFACES DE NERVURE D'AILE CONIQUES


    Contributors:

    Publication date :

    2021-04-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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